P/N: an665-21r
Category: Controls & Cables
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 4 Available |
The AN665-21R is a threaded clevis rod end conforming to AN665 specification for aircraft control linkages. This forked connection point accepts a clevis pin to terminate a control rod or cable at a bellcrank, lever, or control surface. Right-hand threads (denoted by the R suffix) allow secure attachment to threaded control rods.
Installation requires the correct clevis pin size and safetying wire per aircraft maintenance manual procedures. Common in aileron, elevator, rudder, and flap control systems on general aviation and commercial aircraft.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The AN665-21R is a threaded clevis rod end conforming to AN665 specification for aircraft control linkages. This forked connection point accepts a clevis pin to terminate a control rod or cable at a bellcrank, lever, or control surface.
The CLEVIS,ROD END may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: New Surplus. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the CLEVIS,ROD END. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the an665-21r.